# N347QS: 2014 Embraer S A EMB-505

- Status: Valid registration
- Airframe: [Embraer S A EMB-505](https://openairdocs.org/model/embraer-s-a-emb-505) (registry code 326040C, 9 seats)
- Engine: [Pratt & Whitney Canada PW535E](https://openairdocs.org/engine/pratt-whitney-canada-pw535e) (registry code 52297)
- Data sheets: [TCDS A60CE](https://openairdocs.org/tcds/A60CE) (Embraer S.A.), [TCDS E00053EN](https://openairdocs.org/tcds/E00053EN) (Pratt & Whitney Canada Inc.) (OpenAirDocs)
- Serial number: 50500257
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: November 19, 2014
- Certificate issued: April 27, 2026
- Expires: April 30, 2033
- Mode S code: A3D8BE
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=347QS
- Page: https://openairdocs.org/aircraft/N347QS

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 13 in force

### Matched by airframe (Embraer S A EMB-505)

- [AD 2026-10-18](https://openairdocs.org/ad/2026-10-18): Flight Control System · Embraer EMB-505. Effective Jul 6, 2026
- [AD 2026-03-05](https://openairdocs.org/ad/2026-03-05): Autopilot Main Servo · Embraer EMB-505. Effective Mar 31, 2026
- [AD 2024-22-06](https://openairdocs.org/ad/2024-22-06): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Jan 2, 2025
- [AD 2024-17-09](https://openairdocs.org/ad/2024-17-09): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Nov 12, 2024
- [AD 2023-21-04](https://openairdocs.org/ad/2023-21-04): Indicating/recording system · Embraer EMB-505. Effective Dec 11, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-05-12](https://openairdocs.org/ad/2022-05-12): Elevator Structure, Rudder Structure, Ailerons · Embraer EMB-505. Effective Apr 13, 2022
- [AD 2021-24-21](https://openairdocs.org/ad/2021-24-21): Operations · Embraer EMB-500 and EMB-505. Effective Jan 25, 2022
- [AD 2018-07-10](https://openairdocs.org/ad/2018-07-10): Flight Controls · Embraer EMB-500 and EMB-505. Effective May 15, 2018
- [AD 2016-22-02](https://openairdocs.org/ad/2016-22-02): Equipment/Furnishing · Embraer EMB-500 and EMB-505. Effective Dec 1, 2016
- [AD 2014-19-01](https://openairdocs.org/ad/2014-19-01): Landing Gear · Embraer EMB-505. Effective Oct 22, 2014
- [AD 2012-13-04](https://openairdocs.org/ad/2012-13-04): Flight Controls · Embraer - Empresa Brasileira de Aeronautica EMB-505. Effective Aug 6, 2012

### Matched by engine (Pratt & Whitney Canada PW535E)

- [AD 2025-05-13](https://openairdocs.org/ad/2025-05-13): Turbine Section · Pratt & Whitney Canada PW535E and PW535E1. Effective Apr 23, 2025

### Historical (superseded or no longer in force)

- [AD 2023-22-11](https://openairdocs.org/ad/2023-22-11) (historical): Autopilot Main Servo · Embraer EMB-505. Effective Dec 26, 2023
- [AD 2023-21-06](https://openairdocs.org/ad/2023-21-06) (historical): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Dec 11, 2023
- [AD 2020-12-08](https://openairdocs.org/ad/2020-12-08) (historical): Elevator Structure; Rudder Structure; Ailerons · Embraer EMB-505. Effective Jul 1, 2020
- [AD 2013-22-20](https://openairdocs.org/ad/2013-22-20) (historical): Landing Gear · Embraer EMB-505. Effective Nov 8, 2013
- [AD 2011-20-01](https://openairdocs.org/ad/2011-20-01) (historical): Flight Controls · Embraer - Empresa Brasileira de Aeronautica EMB-505. Effective Oct 31, 2011

## Information bulletins (advisory) (2 in force)

- [SAIB CE-16-23](https://openairdocs.org/saib/CE-16-23): Navigation; Degraded Attitude and Heading Reference System (AHRS) Performance When Operating in Areas of Unreliable or Unavailable Global Positioning System (GPS) Signal. Issued Sep 7, 2016
- [SAIB CE-10-46](https://openairdocs.org/saib/CE-10-46): Navigation; Embraer EMB-505 Terrain Awareness Warning System (TAWS) Instructions in Airplane Flight Manual. Issued Aug 16, 2010

## NTSB investigations

None matched to N347QS.

## FAA accident and incident reports

None matched to N347QS.

## Service difficulty reports (11)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2026010506410](https://openairdocs.org/sdr/DXTA2026010506410), Jan 2, 2026: SHROUD. FAULTY. DURING DESCENT AT APPROXIMATELY FL 250 AND 280 KIAS A LOUD BUZZ/HUMM BEGAN. IT CONTINUED THROUGH DESCENT OFF AND ON UNTIL AIRSPEED WAS REDUCED BELOW 200 KIAS. S
- [SDR DXTA2025121206050](https://openairdocs.org/sdr/DXTA2025121206050), Dec 9, 2025: BATTERY. DEFECTIVE. EMERGENCY LIGHTS REMAIN ON AT ALL TIMES WITH THE COCKPIT SWITCH IN THE ARM POSITION. REPLACED BATTERIES. OPS CHECK GOOD. IAW PHENOM 300 AMM 33-52-01
- [SDR DXTA2025090904882](https://openairdocs.org/sdr/DXTA2025090904882), Sep 8, 2025: LIGHT SYS. UNKNOWN. AS WE APPROACHED THE AIRCRAFT TO BEGIN PREFLIGHT WE NOTICED THE EXTERIOR EMER LIGHTS AT THE RIGHT WING ROOT WERE FLICKERING. UPON OPENING THE CABIN DOOR, ALL TH
- [SDR DXTA2025041703051](https://openairdocs.org/sdr/DXTA2025041703051), Apr 11, 2025: CONTROL MODULE. DEFECTIVE. BRK FAIL YELLOW CAS: AFTER POWER UP WE DISCONNECTED THE GPU LIKE NORMAL AND RAN THE AFTER START CHECKLIST. WE RELEASED BRAKE TO TAXI FORWARD, AND MADE IT ABOUT 
- [SDR DXTA2025021202329](https://openairdocs.org/sdr/DXTA2025021202329), Feb 11, 2025: WARNING MESSAGE. FALSE ACTIVATION. A-I WINGSTB FAIL YELLOW CAS: CLIMBING OUT OF KTUL A-I WINGSTAB FAIL CAS ILLUMINATED. RAN QRH, MESSAGE PERSISTED, PERFORMED TROUBLESHOOTING AND CHECKS. OPS CHECK
- [SDR DXTA2024101600849](https://openairdocs.org/sdr/DXTA2024101600849), Oct 14, 2024: FLAP SYSTEM. FAULTED. AFTER TAKEOFF WE RECEIVED FLAP FAIL CAS. FLAPS FAILED IN THE NUMBER 1 POSITION AND DID NOT RETRACT TO 0. WE ACCOMPLISHED THE QRH PROCEDURE AND CYCLED THE FLAPS 
- [SDR DXTA2023112810169](https://openairdocs.org/sdr/DXTA2023112810169), Nov 27, 2023: BATTERY. FAULTED. DURING DESCENT, NOTIFIED BY PAX THE EMERGENCY LIGHTS FLICKERING ON & OFF . LIGHT SWITCH WAS CYCLED & AFTER A FEW SECONDS, BEGAN FLICKERING AGAIN WITH SWITCH IN 
- [SDR DXTA2023062689560](https://openairdocs.org/sdr/DXTA2023062689560), Jun 26, 2023: UNKNOWN. UNKNOWN. TAPPING/GURGLING NOISE FROM PILOT SIDE FLOOR AREA & POOLING WATER IN FLOOR VENTS. MOLDY MILDEW ODOR FROM COCKPIT & CABIN. CONDENSATION TRAPPED AT FLOOR VENTS & 
- [SDR DXTA2023053187550](https://openairdocs.org/sdr/DXTA2023053187550), May 31, 2023: UNKNOWN. UNKNOWN. MAIN DOOR HARDWARE: SILVER PART (MARKED PUSH) OF THE EXTERNAL DOOR HANDLE DOES NOT SPRING INTO THE FLUSH POSITION AFTER USE, INSTEAD IT REMAINS LOOSE AND HANGIN
- [SDR JGVR20200918001](https://openairdocs.org/sdr/JGVR20200918001), Sep 18, 2020: BALANCE WEIGHT. WRONG PART. WHILE COMPLYING WITH SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE PER SB AND REPLACED WITH NEW PARTS. ONE LT ELEVATOR HORN W
- [SDR DXTA201808221274](https://openairdocs.org/sdr/DXTA201808221274), Aug 7, 2018: STARTER GEN. FAILED. DURING CLIMB, FELT AN ABNORMAL VIBRATION. WHILE RUNNING ENGINE ABNORMAL VIBRATION CHECKLIST, THE VIBRATION INCREASED AND GEN 2 OFF BUS MESSAGE DISPLAYED, AND GE

## Service difficulty reports on N347QS not matched to an aircraft (10)

They name N347QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200808073217](https://openairdocs.org/sdr/DXTA200808073217), Aug 7, 2008: CONTROLLER. OUT OF POSITION. CAPT PFD CONTROLLER EJECTED FROM PANEL ON TAKEOFF. TAKEOFF DISCONTINUED SECURED CONTROLLER, OPS CHECK GOOD WORKED IAW MM CH 34-23-02.
- [SDR DXTA200803217](https://openairdocs.org/sdr/DXTA200803217), Aug 7, 2008: CONTROLLER. SEPARATED. CAPTAIN PFD CONTROLLER EJECTED FROM PANEL ON TAKEOFF. TAKEOFF DISCONTINUED. (S)
- [SDR CWQR200703](https://openairdocs.org/sdr/CWQR200703), Jul 6, 2007: ATTACH BRACKET. CRACKED. DURING A PHASE 1-4 INSPECTION, FOUND THE MASTER CYLINDER ATTACH BRACKET MOUNT HOLES GOUGED DURING INSTALLATION AT THE FACTORY, UPON FURTHER INSPECTION FOUND A .
- [SDR DXTA200701961](https://openairdocs.org/sdr/DXTA200701961), Feb 22, 2007: ACTUATOR. INTERMITTENT. RH MAIN GEAR LIGHT WOULD NOT ILLUMINATE AFTER 2 CYCLES OF LANDING GEAR. AFTER GO AROUND AND VERIFICATION FROM TOWER WAS RECEIVED, RIGHT HAND GEAR LIGHT ILLUMINA
- [SDR DXTA200701926](https://openairdocs.org/sdr/DXTA200701926), Feb 8, 2007: STRUT. DISCHARGED. DURING GEAR EXTENSION , DID NOT ACHIEVE A GREEN( LOCKED INDICATION) ON THE RIGHT MAIN GEAR. RAN THE GEAR WILL NOT EXTEND CHECKLIST. GEAR WAS DOWN BUT NOT LOCKED
- [SDR DXTA200601782](https://openairdocs.org/sdr/DXTA200601782), Dec 6, 2006: SWITCH. OUT OF ADJUST. (CABIN DOOR) ANNUNICATOR ILLUMINATED DURING T/O AT 70 KNOTS. ABORTED T/O ROLL. ADJUSTED MAIN CABIN DOOR LOCK SWITCH. OPS CHECKS GOOD IAW MM 52-70-01.
- [SDR DXTA200601723](https://openairdocs.org/sdr/DXTA200601723), Nov 11, 2006: SOLENOID. INOPERATIVE. RT ENGINE ITT REACHED 730 DEGREES (C) FOR APPROX 3 SECONDS DURING TAKEOFF ROLL; TAKEOFF ABORTED. N1 WAS EXACTLY AT TARGET FOR CONDITIONS. REMOVED AND REPLACED B
- [SDR DXTA200601424](https://openairdocs.org/sdr/DXTA200601424), Jun 4, 2006: COALESCER BAG. DIRTY. DURING FLIGHT, MODERATE ELECTRICAL ODOR IN CABIN, ESPECIALLY ALONG CEILING AREA NEAR DOOR. NO VISIBLE SMOKE. ODOR DISAPATED DURING DESCENT. CONDITIONS: FL400, N
- [SDR DXTA200501084](https://openairdocs.org/sdr/DXTA200501084), Nov 14, 2005: ODOR. DETECTED. DURING DESCENT, WINDSHIELD HEAT WAS SELECTED TO LOW, AFTER OPENING THE WINDSHIELD BLEED KNOBS. APPROX 1 MINUTE LATER AN ODOR WAS OBSERVED FOLLOWED BY THE -WINDS
- [SDR DXTA200500858](https://openairdocs.org/sdr/DXTA200500858), Jul 24, 2005: DOWNLOCK SWITCH. INOPERATIVE. ON TAKEOFF, RIGHT MAIN GEAR WOULD NOT COME UP (HANDLE DID). FOUND ACTIVATING SIDE OF RT UPLOCK SWITCH BAD. REMOVED AND REPLACED SWITCH IAW 560M/M CHPT 32-31-05.

## STCs that may be installed (OpenAirDocs) (47)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Embraer S A EMB-505)

- [STC SA12141IB](https://openairdocs.org/stc/SA12141IB): GOGO HDX antenna systems integration. FTI ENGINEERING NETWORK GmbH
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04761NY](https://openairdocs.org/stc/SA04761NY): True Blue TS56 Emergency Battery Power Supply Replacement. Mid-Continent Instrument Co. Inc
- [STC SA12286AT](https://openairdocs.org/stc/SA12286AT): Installation of a LEO Connectivity System. Embraer Engineering & Technology Center, USA, Inc
- [STC SA12143CH](https://openairdocs.org/stc/SA12143CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA02779SE](https://openairdocs.org/stc/SA02779SE): Installation of Gogo AVANCE L3 Inflight Connectivity System. AeroMech Incorporated
- [STC SA12140IB](https://openairdocs.org/stc/SA12140IB): Mechanical provisions for the installation of a GOGO HDX antenna. FTI ENGINEERING NETWORK GmbH
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA09942AC](https://openairdocs.org/stc/SA09942AC): Installation of Schatz Bearing Corporation, Radial Bearing P/N’s : KP60BHT-H-OPG and KP64BHT-H-OPG. AV8 PMA LLC
- [STC SA00087IB](https://openairdocs.org/stc/SA00087IB): Medical reconfiguration of the EMB-505. UMLAUT ENGINEERING GMBH
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA04552AT](https://openairdocs.org/stc/SA04552AT): Installation of cargo compartment floor covering. Embraer Engineering and Technology Center, USA, Inc
- [STC SA04548AT](https://openairdocs.org/stc/SA04548AT): Installation of an Avionica, LLC Quick Access Recorder/Data Concentrator model avRDC MAX (QAR) P/N 804-1250-32 and optional Avionica, LLC Cellular Module LTE (avCM LTE) P/N 650-0100-05. Aircraft Systems and Manufacturing Inc
- [STC SA00038IB](https://openairdocs.org/stc/SA00038IB): Replacement of the Passenger Seat Cushion Covers and Foams on the Embraer S.A. EMB-505. Waypoint Aerotec Limited
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA01727WI](https://openairdocs.org/stc/SA01727WI): Interior Alteration for Installation of a Coffee Maker and Modification of No Smoking Signs. Netjets Aviation Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA04463AT](https://openairdocs.org/stc/SA04463AT): Installation of a Gogo Business Aviation Avance L5 Air To Ground (ATG) In-Flight Entertainment and Connectivity (IFEC) System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03010CE](https://openairdocs.org/stc/SA03010CE): Installation of a Lacobucci HF Electronics Nespresso Machine PIN HFE96-28T-10 and/or Monogram System -TIA Division Wavejet Microwave Oven PIN 400-1860-01. Embraer Engineering & Technology Center - USA Inc
- [STC SA04397NY](https://openairdocs.org/stc/SA04397NY): Installation of Satcom system. 328 Support Services GmbH
- [STC SA03003CE](https://openairdocs.org/stc/SA03003CE): Installation of an Aviator 200 Satcom System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03005CE](https://openairdocs.org/stc/SA03005CE): Installation of an Aviator 200 Satcom System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03001CE](https://openairdocs.org/stc/SA03001CE): Installation of Honeywell High Frequency (HF) Communication System, model KHF1050HF, and AvTec Selective Calling (SELCAL), model CSD-714. Embraer Engineering & Technology Center - USA Inc
- [STC SA03006CE](https://openairdocs.org/stc/SA03006CE): Installation of a Medical Evacuation Configuration (Medevac). Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA00959DE](https://openairdocs.org/stc/SA00959DE): Installation of Concorde valve regulated Lead-Acid batteries in replacement of aircraft main batteries. Concorde Battery Corporation
- [STC SA00901DE](https://openairdocs.org/stc/SA00901DE): Installation of up to Two Exxternally Mounted Gimbal Systems. Straight Flight Inc
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA03004CE](https://openairdocs.org/stc/SA03004CE): In accordance with Part 23 regulations specified in the current certification basis of Type Certificate Number A60CE, installation of pilot's new, extended seat tracks. Embraer S.A
- [STC SA03956AT](https://openairdocs.org/stc/SA03956AT): Installation of Aircell ATG-4000 High Speed Internet System (AHSI) and Aircell Axxess II Iridium Satcom or Aircell Aviator 200 SBB Satcom, Aircell ATG 5000 High Speed Internet System (AHSI) all with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS
- [STC SA03764NY](https://openairdocs.org/stc/SA03764NY): Installation of the Low Gain Satcom Antenna. Roeder Praezision GMBH
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC SA04278AT](https://openairdocs.org/stc/SA04278AT): Installation of a cabin In-Flight Entertainment & Passenger Audio System. Embraer Engineering & Technology Center - USA Inc
- [STC SA04145CH](https://openairdocs.org/stc/SA04145CH): Installation of a cosmetic threshold in the aft baggage compartment to protect interior coverings/materials from loading and removal of baggage. Elliott Aviation Technical Products Development, Inc
- [STC SA04260AT](https://openairdocs.org/stc/SA04260AT): Installation of an 802.11 Wireless Internet System. Embraer Engineering & Technology Center - USA Inc
- [STC SA04243AT](https://openairdocs.org/stc/SA04243AT): Installation of AFT Lavatory Coat Hanger Support. Embraer Engineering & Technology Center - USA Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA03352CH](https://openairdocs.org/stc/SA03352CH): Activation of an 802.11 a/b/g and n Wi-Fi System. Elliott Aviation Technical Products Development, Inc
- [STC SA01789WI](https://openairdocs.org/stc/SA01789WI): Quasar II Cabin Lighting with eConnect and Noise Mitigation. Duncan Aviation Inc
- [STC SA01760WI](https://openairdocs.org/stc/SA01760WI): Installation of an Aircell Universal Cabin System (UCS) 5000 with Wireless Local Area Network (WLAN). Duncan Aviation Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA01703WI](https://openairdocs.org/stc/SA01703WI): Installation of Concorde RG-380E/44 and RG-390E VRSLA Batteries. Concorde Battery Corporation
- [STC SA01692WI](https://openairdocs.org/stc/SA01692WI): Installation of Aircell High Speed Internet (AHSI) System with Wireless Local Area Network (WLAN) capability. Duncan Aviation Inc

## Related

- Other Embraer S A EMB-505 aircraft: https://openairdocs.org/model/embraer-s-a-emb-505/aircraft.md
- The Pratt & Whitney Canada PW535E engine: https://openairdocs.org/engine/pratt-whitney-canada-pw535e.md

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